Implement and facility for capturing grounding missiles and penetrating missiles in a fixed point and collecting guiding rockets and aircrafts and manufacture method thereof

ABSTRACT

Disclosed are a device and a method for discharging energies of an energy carrying device when impacted in an open space. By the present invention, static energies of the earth absorbs potential energies of human science and technology products, and the eruption and destruction become a gradual leakage in the local confrontation. The mechanisms provided by the embankment mortise stack facilities, the fixed rod implements and the mortise sampan transporters provide intelligent and procedural measures for collecting missiles, penetrating missiles, rockets, spacecrafts and satellites, so that the missiles and penetrating missiles that attack the ground are collected, and the space devices such as rockets, spacecrafts and satellites are collected from space to ground, and cause no damage.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of priority from Chinese PatentApplication No. CN201811275119.4, filed on Oct. 19, 2018. The content ofthe aforementioned application, including any intervening amendmentsthereto, is incorporated herein by reference in its entirety.

TECHNICAL FIELD

The defense and capture technology of ballistic missiles, cruisemissiles and penetrating missiles; the ground collection technology ofspace rockets, airship and satellites.

By the present invention, the intelligent missiles of the attackingparty can be rejected in the war; the program missiles in the attack arefrequently captured; the saturated attack of the missiles can becollected in the type of umbrella; the sudden attack of attacking partyto the command hub is tactically aborted; the missile that escapes thespace missile defense system is turned to be captured on the ground.

In the construction, the spacecraft equipment such as rockets,spacecrafts and satellites are turned into space shuttles and arecollected and reused.

The collecting method of machines or non-machines is applicable tospacecrafts of various forms and different orientations of spacecrafts.

BACKGROUND

The background of the present invention is “inverted fastening mortisebuilding structure for resisting earthquake, strong wind and tsunami andtechnical procedure thereof” according to Chinese Patent ZL201310465498.4.

SUMMARY

In the present invention, provided is an energy discharging implement inan open space for an energy carrying space device. The energydischarging implement comprises a fixed rod, an implement and anembankment mortise stack; the fixed rod which is a top-down bracketsupporting implement comprises a frame bracket rod with a base, a framebracket rod, a bracket rod sleeve, a bracket top cover; the implementcomprises a loading missile frame comprising a supporting shaft, abearing sleeve, a support shaft bearing, a fixed bearing device, abearing fixing nut, a guide rod, a guide rod bearing, a guide rodhanging piece, a diagonal sliding hole cover, a fixed hanging body, aframe bracket fixing plate, a frame bracket bottom plate, a springnarrow steel plate, a nylon rope net for picking up and changing thetrajectory of thrown loading missiles, changed missiles, accepted cruisemissiles, ballistic missiles and penetrating missiles; the embankmentmortise stack comprises mixed mortises, slippery mortises and separationmortise boards; the mixed mortises are mortise stones covered on asurface of the stack with mortises with four diameters of φ12 cm, φ8 cm,φ4 cm, and wheat grain mortises which are layered orderly with 30 cm ineach layer; the slippery mortises are mortise stones with φ12 cm andlayered orderly in every layer of 3 m covered in the stack in the innercircle; the separation mortise board is a modular high-strengthdouble-layer reinforced concrete slab or a high-strength fire-resistantglass steel sheets placed between different mortise layers; the stack isconfigured to catch missiles thrown by the loading missile frame or themissiles that are directly attacked; the set separation mortise boardsin each layer have different seams and sizes, and right and left sidesof each layer are asymmetric, and the set separation mortise boards ineach layer which are not jointed are superimposed; the mortise sampantransporter further comprises mortise floating prying shoes, climbingclaw shoes and covers; the implement and the embankment mortise stackare integrated to collect rockets; structures and mechanisms ofrespective energy carrying devices fit surface tensions and frictioncoefficients of mortises, which consume energy of the energy carryingdevices, so that the energy carrying devices are collected.

The vis inertiae of the original storage on earth and the active forceof moving equipment such as missiles, penetrating missiles, rockets, andspacecrafts developed by human science and technology are mutuallyintertwined in the local confrontation. The detonation procedure causedby the missile' impact is circumvented in the process; the energyconcentrated in the impact is dispersed; and the original trajectory ofthe equipment is changed, so that the intelligent missile loses theoriginal tactical target, and the program missile is captured afterexhausting the energy thereof. Thus, the rocket and the spacecraft arecollected without the impacting damage.

In the present invention, the slight surface tension of themachine-adapting mechanism of embankment mortise stack and the slightfriction between mortises and stone mortises inherit and disposepowerful impact waves from missiles, penetrating missiles, rockets andspacecrafts, so that the kinetic energies carried by the impact wavesare consumed by themselves when inheriting and disposing the powerfulimpact waves. Therefore, the impact waves are dissipated in thecoordination process of the mechanism by the friction and surfacetension of the embankment mortise stack. The static energy of the earthneutralizes the technological potential energy of the device, so thatthe above-mentioned equipment is collected by changing the trajectory.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1-3 schematically show matching parts of a fixed rod implement,where: 1, supporting shaft; 2, bearing sleeve; 3, supporting shaftbearing; 4, fixed bearing device; 5 bearing nut; 6, guide rod; 7, guiderod bearing; 9, guide rod hanging piece; 9, diagonal sliding hole andcover piece; 10, fixed hanging body; 11, loading missile frame; 12,frame bracket rod; 13, bracket rod sleeve; and 14, bracket top cover(14).

FIGS. 14-26 schematically show respective combinations of graded mortiselayers and separation mortise board layers in embankment mortise stack;where: 15, seat mortise layer of embankment mortise stack; 16,separation mortise board layer of embankment mortise stack; 17, gradedmortise layer of embankment mortise stack; 18, graded separation mortiseboard layer of embankment mortise stack; 19, permissive separationmortise board layer of embankment mortise stack.

FIGS. 27-39 schematically show different functions and comprehensiveeffects of the loading missile frame facility and the embankment mortisestack implement which accept and capture cruise missiles, ballisticmissiles and penetrating missiles from different positions, differentpositions and different orientations when the embankment mortise stackimplement and the fixed-rod loading missile frame are combined.

FIG. 40 is an enlarged view of a bracket, a sleeve, a frame bracket seatand a fixing bolt, in which a pre-set separation mortise boardrepresents a smooth board, and an in-site cast separation mortise boardrepresents a rugged board.

FIGS. 41-46 schematically show defense drawings of the attack anddefense of the missile of invisible mortise stack, aiming at the missileand the penetrating missile that are not exhausted.

FIGS. 47-65 schematically show matching parts of a travellingtransporter; where: 45, mortise sampan; 24, sampan; 25, sampan tip; 28,sampan axle; 29; sampan rudder; 32, anti-reverse ring; 10, fixed hangingbody; 11, loading rocket frame; 12, frame bracket rod; 26, floatingmortise board of travelling sampan; 27, sling hole; 30, umbrella ribwheel; 32, energy guide rod; 32, energy guide wheel; 33, acute anglepry; 34, long short hammer; 35, straight rod hammer; 36, flat plow; 37,sharp plow; 38, bald plow; 39, straight angle pry; 40, mortise drapingrake; 41, mortise combing rake; 42, mortise separating hammer; 43,hammer with different rods; 44, hammer with short rods; 46, energy guideconnecting rod; 47, bracket fixing rod of tip net; 48, tip net.

FIGS. 66-79 schematically show travelling states of the travellingsampan when collected with spacecrafts such as rockets and satellites,and travelling lines of rockets which drop out the mortise sampan due tofaults of storage lanyards and navigation hubs which are pre-positioned.

Main functional components and functional structures in the accompanyingdrawings are numbered; and the thin solid line in the accompanyingdrawings is a function marking line; the thin solid line at the bottomof the accompanying drawings is a line for combining drawings; thedotted line is a rocket thrown line; the solid arrows in the drawing aretrajectories of missiles, sampans and rockets; the dotted line diagramsare shapes of objects that lose positions thereof; the thick dashed linein the drawing is a logical line of an aircraft instead of a geometricline; the travelling lines of the missiles and rockets and the rocketthrown lines in the drawings are all logical lines instead of measuredlines.

DETAILED DESCRIPTION OF EMBODIMENTS

A fixed rod implement of embankment mortise stack is designed accordingto the consistency principle of the missile, frame, and stack. The frameis square, and the length of the missile is the same as the length andwidth of the frame. The length of the setting frame is N m, the diameterof a corresponding frame supporting shaft is also N m and the diameterof a guide rod steel pipe is 0.4 times than N m, which are the referencevalue of the quantity.

The frame supporting shaft equipment including a steel pipe, a supportshaft bearing, a bearing sleeve, a fixed bearing device and a bearingfixing nut is prepared; and both ends of the steel pipe are processedwith threads.

The guide rod steel pipe with the same length of the frame width isprepared, and the matching parts of the guide rod steel pipe such as aguide rod bearing, a guide rod hanging piece, a diagonal sliding holecover and a fixed hanging body are also prepared.

The high-strength flame-retardant resin and high-quality fiber cloth areused to mold a loading missile frame which the bracket fixing plate isas thick as the frame supporting plate, and the support is made firstlyand then the frame is made. The width and upper edge height of the framebracket fixing plate are one tenth of the frame length, and the loweredge height is six percent of the frame length. The upper and lowerparts are combined with the frame supporting plate, and the height ofthe frame bracket rod mold also includes the thickness of the frameplate. The upper center of the sliding hole of the frame bracket islocated at a position which is four tenths along the middle line at theupper edge; the lower center is located at a position which is ninetenths along the middle line at the upper edge and is located at aposition which is three tenths along of the middle line; the two circlesare connected to form a diagonal sliding hole. A support shaft hole islocated at a position which is two thirds along the middle line at thelower edge, and both holes use an end diameter of the support shaft asdiameters.

After the frame bracket fixing plate is completed, the supporting shaftsteel pipe is inserted in time. The parts of the bracket and frameconnected to the supporting shaft are coated with the resin and thefiber cloth until the diameter of the parts is twice to the originaldiameter. The frame bracket fixing plate is molded, and the surface sidehas horizontal fixing holes; the template is removed in time to positionthe supporting shaft into the frame, and the resin and the fiber clothare coated between the frame supporting plate, the frame bottom plateand the supporting shaft to form a connected body.

The prefabricated spring narrow steel plate is fixed to the front andrear ends of the surface sides of the frame, and the left and righttransverse sides of the front and rear horizontals of the spring steelplate and the frame bracket fixing plate are vertical placedcorrespondingly, and left and right transverse sides and surfaces sidesare provided with round holes which is used as a net fixing point andare surrounded.

After the bearings, hanging pieces and pin parts are assembled at bothends of the guide rod, the above combination is wrapped and reinforcedwith the same resin and fiber to twice the original diameter, and thesurface can be rough. After curing, the hanging piece is matched, thebearing is inserted into the rod to fix the device with a pin. Theremaining position is biased to the hanging piece, and the hanging pieceand the bearing are sealed with beef tallow, and the diagonal slidinghole installed in the loading missile frame is covered with the cover.The fixed hanging body is fixed on the bracket fixing plate of theloading missile frame, which is on the same side of the diagonal slidinghole. Around the frame, the frame bracket fixing plate, the spring steelplate and the horizontal fixing holes are used as a fulcrum, and thehigh-performance nylon rope is used for weaving networked pockets.

A frame bracket rod with the seat, a bracket rod sleeve, a bracket rod,and a top cover of the bracket rod are molded, in which the fixed holesexist between each other.

Separation mortise boards include prefabricated separation mortiseboards and in-site cast separation mortise boards, and are made ofhigh-strength fire-resistant glass steel sheets and double-layerreinforced concrete slabs. The thickness of the glass steel sheets andthe reinforced concrete slabs respectively are 3-5 cm and 7-12 cm, andthe single plate area is 4 m² as the reference data, and the plates ofthe same plane are asymmetrical, non-identical and complementary.

Embankment mortise stack in strategic hub for preventing fallingmissiles is centered on the hub, and the periphery is shaped like acircle, in which the inner ring is covered with φ12 cm of the samestandard mortises from the inside to the outside and the outer peripheryis 1 m of the width as an earth embankment. Four kinds of mortises suchas φ12 cm, φ8 cm, φ4 cm, and wheat grain mortises are layered orderly inevery layer of 30 cm, and after a stack with a single material insideand a mixed material of outside is added to a height of 3 m, thescaffolding is set. In addition to the conventional protection tools,operators wear mortise floating prying shoes into mortises foroperation. The prying shoe is a combination of pries and shoes. Thepries and the shoes are tightly jointed at a toe web part, and the priesand the shoes are loosely jointed at a tendon part. The front, back,left and right sides of the pries are three times the size of the shoes,and the shoes are installed in the middle of the pries.

After tidying the seat mortise layer, prefabricated or cast-in-placeseparation mortise boards are placed in the mortises, wherein thecast-in-place part of reinforced concrete is divided into four parts.The cast-in-place method of modular 1 is that the perimeter isreinforced by three-ply woods, then the mortise layer is tidied, and theplastic film is spread. The concrete is poured into the mortise from theperiphery to the center. After tidying the concrete, the bottomreinforcing steel bars are placed. Then the concrete, the surface layersteel reinforcing steel bar and surface layer concrete are added. Theaddendum is tidied and pressed by a roller, then compacted by a flatjarring machine. The product is cured and cut by the design of theoriginal plate surface, and after nine tenths of the product is cut, theremainder is naturally broken. The cast-in-place method of modular 2 isthat the mortise layer is separated by wooden strips according to theset module and the wooden strips are fixed in a connection. Theseparated module and wood strips are covered by films integrally. Themortise is tidied successively and cast jointly layer by layer in theform of full basin, and then the mortise is tidied uniformly. Afterproduct is tidied, pressed by the roller and reinforced by the flatjarring machine, the wood strips break naturally. The cast-in-placemethod of gridding 3 is that a grid weaved is moved by straw ropesaccording to the setting requirements into the surface mortise. Afterthe straw ropes are lifted appropriately by three-ply woods, the mortiseis tidied and covered by films integrally. The concrete is transportedinto the mold by the rope as a pilot in the entire basin. The concreteis tidied and the bottom reinforcing steel bars are placed. Theconcrete, the surface layer steel reinforcing steel bar and surfacelayer concrete are added. If the height is not enough, the straw ropesare added twice and tied by wire. The mortise is covered by films againand cast additionally. The cast-in-place method of supplementary absence4 is that the pre-set separation mortise board is placed in the mortisealternately. After vacancies separated by wooden strips, the mortise istidied and covered by films integrally. Then the reinforced concrete isadded and cast. The last three methods do not need a cutting process.

Seamless joints in the same layer are not required, and the upper andlower sections need to be connected alternately. After several layers,the frame bracket rod with a base is moved to the separation mortiseboard and fixed according to the set position. When every layer isplaced, the position of the frame bracket rod needs to be correcteduntil accumulated to a mixed mortise layer on the top; and when theheight of the frame bracket rod is insufficient, the sleeve is used forconnecting.

The operation of a glass reinforced plastic separation mortise board isthe same as the reinforced concrete separation mortise board. When themortise is cast, the surface needs to be tidied, and when the castingarea is cured to 30% to 50%, the glass reinforced plastic is moved tothe casting area. A pre-set separation mortise board is called a smoothboard, and a cast-in-place separation mortise board is called a ruggedboard. In the conventional medium, the smooth board and the rugged boardare placed alternately, or vacancies are added by two types of boards inthe same layer.

The sand with a high sedimentation rate is poured into the frame bracketrod according to different settings, and the water is injected into therod mouth to promote precipitation; or the slurry mixed by buildingstone powder and clay or the proportional steel and concrete are pouredinto the frame bracket rod, and the latter two needs vibration by avibrating rod.

Related parts are hoisted. After the fixing the loading missile frame,the frame bracket rod mouth is covered by the top cover and the guiderod is suspended on the upper end of the diagonal sliding hole by thehanging block. The force from the frame hanging ring is limited andgathered by four ropes of the same length, and the hanging body is hungto orient the frame.

As shown in FIGS. 31 and 34, a missile which enters the loading missileframe from the implements of embankment mortise stack can hit any partof the frame, and then the missile loading frame becomes a missilechanging frame which transforms the straight energy of the missile intoa circular motion, and returns the impact energy of the missiles fromthe tail feather to the missile to prompt the speed of the tail toexceed the body and the warhead, and the missile is thrown in the formof a parabolic; therefore the detonation procedure triggered by theoriginal impact of the missile is removed. The missile slides and fallsfrom the slope of the stack, and φ12 cm and φ8 cm of the large standardmortises in the mixed mortises ploughed by the tail feather are nakedand fell, which can support the falling of the missile and dissipate thefriction of the missile, and convert friction into heat. The sediment ofthe small standard mortises becomes a furrow of the missile.

As shown in FIGS. 28 and 29, a falling point missile which fallsdirectly to embankment mortise stack without touch of the loadingmissile frame. Due to the increased resistance of the frictioncoefficient and the push of the rear force of the missile body in theloose friction along the mixed mortises, the speed of the tail exceedsthe warhead, and the missile is thrown in the form of the sameparabolic. Then the missile slides and falls along the slope to plow outthe furrow, and the original impact of the missile is removed.

As shown in FIGS. 30, 31 and 32, the cruise missile that strikesembankment mortise stack vertically, passes through the loose mortiselayer of the stack. Due to the passageway formed by the smoothseparation mortise board and the rugged separation mortise board, thetrajectory of the missile is changed, the missile is driven forward byresistance and consumes energy due to friction. Then the missile drillsout along the established structure of the stack, and the originalimpact of the missile is removed due to the loss of impact.

As shown in FIG. 35, a penetrating missile with gravity wave andacceleration of a tail-spray strikes embankment mortise stackvertically. After the friction coefficient of the missile is reduced andthe trajectory of the missile changes by the mixed mortise layer ofembankment mortise stack, the penetrating missile with acceleration of arocket tail spray avoids an explosion by shuttling the slippery mortiselayer of the separation mortise board of the stack.

As shown in FIG. 36, a penetrating missile with high-energy strikes theloading missile frame vertically. The energy carried by missile changesthe frame into a circular motion without gaps, and then the missileautomatically falls and avoids an explosion after the energy isexhausted.

As shown in FIG. 37, a penetrating missile strikes the face of theloading missile frame vertically which is thrown to the slope of themixed mortises of embankment mortise stack due to the slip of the frame,so that the missile has no impact and avoids an explosion.

As shown in FIGS. 38 and 39, a touch spot missile without reward of asame energy strikes the middle of the loading missile frame vertically,and the warhead is guided by the guide bar to a side and obtain the sameenergy to renewal, and then the missile is thrown and avoids anexplosion due to lose the impact.

As shown in FIG. 33, the missile sliding down the slope and the floorsurface, which passed by the loading missile frame is captured after theenergy of the missile is consumed.

A hidden mortise facility of embankment mortise stack which the mode isto remove the loading missile frame and the frame bracket rod uses thesame procedure in the facility of the stack, where a separation mortiseboard is placed in a fragmented manner; a steel plate or a scrap steelplate with the anti-rust treatment is used as a smooth board for aseparation mortise board, and a cast-in-place reinforced concrete slabor a glass steel sheet is used as a filled and septal rugged board, andif necessary, the steel plate may be longitudinally thickened with steelstrip to fill with the same thickness as the mortise board, theabove-mentioned materials are used to constitute and accumulate thefacility of the stack. Transferred strategic hubs are still input intoinformation flow and signal sources of the hubs, which are closelydistributed in non-strategic defenses for tactical deception andtemptation, so that saturation-attack rain missiles formed bypenetrating missiles, cruise missiles and ballistic missiles areumbrella-type collected. The mode not only relieves the tactical attack,but also directly deciphers all the technical parameters of catchingprocess.

As shown in FIG. 41, the penetrating missile striking from the top ofembankment mortise stack is accept by the irregularity of separationmortise boards and blocked by mortise layers due to friction. Theleakage of the tension of the mortise and the drift of the separationmortise board lead the missile to drift and change the trajectory. Thepenetrating missile is introduced into the separation mortise boardlayer and drilled out.

As shown in FIG. 42, after striking the slope foot of mixed mortiselayers of embankment mortise stack changes the trajectory, thepenetrating missile which is pushed and forced caused by the rocket tailspray from a passageway formed by a floor and a separation mortise boardlayer is captured.

As shown in FIG. 43, the cruise missile passing by the slope slidesalong a slope and a floor, and the cruise missile is captured after theenergy of the missile is exhausted.

As shown in FIG. 44, the cruise missile striking from the side top ofembankment mortise stack is blocked by friction of the mixed mortiselayer. The cruise missile carries the rocket tail spray and flies to theair after turning around in weightlessness of a tail and a head.

As shown in FIG. 45, a ballistic missile without endurance energystrikes from the side top of embankment mortise stack in a same part.The missile is blocked by friction of the mixed mortise layer and theslippery mortise layer and thrown conversely. The missile becoming agliding missile to slide continuously is captured after the energy ofthe missile is exhausted.

As shown in FIG. 46, the missile striking a separation mortise boardlayer of embankment mortise stack vertically is forced to change thetrajectory and glides through a slippery mortise layer. Then the missileis captured after the energy of the missile is exhausted.

A mortise sampan transporter of embankment mortise stack is produced allparts of the mortise sampan and embankment mortise stack in FIGS. 47-65according to the settings. The mortise sampan is assembled according tothe outline of the collected aircraft and the mechanism of the fixed rodloading missile frame. The basics and procedures of the frame bracketrod and the loading missile frame are retained, and the loading missileframe changes a loading rocket frame.

The left and right of sampans are molded. The upper side of the sampanis 1.15 times the length of the frame, and the lower base of the sampanis 1.05 times the length of the frame. The height of the bottom of thesampan and the side is slightly higher than the height of the frame. Theupper edge of the sampan is referenced by 2 times the height of theframe as the radius circle of the sampan tip, and the lower edge of thesampan is 2.7 times the height of the frame as the radius circle of thesampan tip. The intersection of the two arcs is the tip of the sampantip, and the inner width of the sampan is 1.08 times the frame.

The left and right of the two sides of solidified sampan are fixed, andthe sampan tip is surrounded by three-ply woods in the type of liftingthe bottom hermetically. After the corresponding mold core is placed atthe sampan rudder ditch and the sling hole, the gel coat is covered, andthe bottom of the sampan is repeatedly coated with the resin and thefiber cloth to connect the left and right sides until the setspecification is reached. After curing, the sampan is turned over, thebottom splint is removed, and the four flat angles of the cabin, thesling hole and the sampan rudder ditch are supported by a support whichis made besides being stable, the mold core of original surfaceprotrusions at the sampan rudder ditch and the sling hole is reversed tothe bottom, and the bottom of the sampan is repeatedly coated with theresin and the fiber cloth until the set specification is reached again.

The frame bracket seat rod of single throw side seat foot is producedmeanwhile. The sampan rudder is made of rust-proof steel plate or metalplate. The upper edge of the rudder has sampan fixed holes, and the sideedge of the rudder wheel fixed holes. The length and thickness of therudder are the same as the rudder ditch, and the height of the rudder is1.6 times the sampan, including the rudder ditch portion. The lower edgeof the rudder is less than 2-3 cm and is properly treated to eliminatethe corners; the bottom length of the rudder is one tenth of the fulllength; the upper slant angle of the rudder is about 12 degrees, and theends are symmetrical.

An umbrella rib wheel is molded, which the outer edge is thin withoutcorner angles and the inner rib spokes and the hub are thick; the ribsof the spokes extend radially outward. The radius of the wheel which ismade of fiberglass must not exceed the height of the sampan.

After the umbrella rib wheel is fixed on the sampan axle by a gasket, abearing, a nut and a pin, two flexible hoops are placed in the center ofthe axle. The hoop has a fixed hole at the bare end, and the hoop baredthe fixed hole is wrapped and reinforced with the resin and fiber totwice the axle diameter. Both ends of the rudder are connected with thehoop of the sampan axle, the sampan is moved in time, and the rudderenters the ditch. The sampan, the sampan axle, the bottom floatingpanel, the rudder, the rudder ditch are adhered with the resin and thefiber cloth. After curing, the body of a mortise sampan is turned overand supported the four corners by a support. The short round steel isinserted into the fixed hole of the rudder as a pin, and wooden stripsare placed at the two edge of the bare rudder and covered by gel coat.The upper edge mouth of the rudder mold pinned is coated and filled withthe resin and the fiber cloth until the rudder mold is filled up. Aftersolidification, the mold is removed, and the rudder, the sampan axle andthe mortise sampan are integrated.

The frame bracket rod seat is fixed into the mortise sampan. In additionto the bottom fixed seat, the frame bracket rod and the sampan are fixedwith the resin and the fiber cloth.

The hoisting loading rocket frame is fixed on the mortise sampan; thetop cover of the frame bracket is installed, and the inner side of theframe hanging ring is welded with a short round steel to form ananti-reverse ring.

Then a fiberglass energy guide wheel and a metallic energy guide rod areproduced and installed synchronously, and an energy guide connecting rodis produced with the same type of steel pipe of the guide rod and thelength of the inner diameter of the sampan; the rods are fixed with theresin and fiber to twice the original diameter, and connect the energyguide wheel on both sides.

A bracket solid rod of a sampan tip net at the upper side arc of thesampan tip is made of steel with the same material as the energy guiderod, a sampan tip net is weaved with nylon ropes between the solid rodand the tip.

According to the setting needs of the removing program of the separationmortise board in a mortise sampan of embankment mortise stack, an acuteangled pry attaches one of the group comprising a hammer with differentrods, a hammer with same rods, a flat plow, a sharp plow and a bald plowto form an acute angle pry plow (hammer), or a straight angled pryattaches one of the group comprising a mortise draping rake, a mortisecombing rake, a mortise separating hammer, a hammer with different rods,a hammer with short rods to form a straight angle pry plow(hammer). Anacute angle pry plow (hammer) and a straight angle pry plow(hammer) arepre-placed in every layer or in a single layer in the stacking ofembankment mortise stack; storage lanyards are leaved between multilayerpries and a pry and a sampan and then the lanyards are pulled out; whenapproaching the top of the stack, the navigation hub equipment is placedin the top of the mortise stack; the mortise sampan is hoisted by ahelicopter or a derrick boom on the top of the mortise stack to seat.The lanyard which is extended from the sling hole penetrates the pendantand lifts the guide rod. The mortise sampan is supported by the floatingload of the mortise and the friction against the rudder.

After taking the rocket, the mortise sampan becomes a travelling sampan.The friction of the sampan on the mixed layer and slippery mortise layerof embankment mortise stack makes the load of the sampan. The acuteangle pry plow (hammer) further increases the friction against themortise sampan, which is collected after running out of energy from thehillside to the flat optionally; or the sampan which the energy isexhausted in the specified local area is collected due to the load isincremented step by step by multiple sets of the straight angle pryplow(hammer).

As shown in FIGS. 68 and 69, when the rocket falls on the left side ofthe loading rocket frame, the mortise sampan is tilted to the left, andthe rudder sinks in the mixed mortise layer to steer and rub, andbecomes a travelling sampan to go down the slope.

As shown in FIGS. 70 and 71, when the rocket falls on the center of theloading rocket frame, the guide rod slides down and guides the head, thebody and the tail of the rocket, so that the rocket tilts to the right,and the rudder sinks in the mixed mortise layer to steer and rub, andbecomes a travelling sampan to go down the slope.

As shown in FIGS. 72 and 73, the rocket falls on the left side of thesampan tip net due to inaccurate navigation, the mortise sampan whichbears potential energy of the rocket goes down the slope to the left orright quickly.

As shown in FIGS. 74 and 75, the rocket falls on the left side of theloading rocket frame due to inaccurate navigation, after the loadingrocket frame transmits energy to the sampan tip, the sampan plows themortise layer to the left.

As shown in FIGS. 76 and 77, the rocket falls on the slope of embankmentmortise stack in front of the left side of the mortise sampan due toinaccurate navigation, and then the rocket slides along the slope intothe flat.

As shown in FIGS. 78 and 79, the rocket falls on the front slope ofembankment mortise stack vertically due to inaccurate navigation, themarch forward of rocket changes the original state of the stack and thestability of the mortise sampan, and breaks through the slipped mortisestone of the stack.

After the above three groups of embankment mortise stack are finished,the surface is covered with building stones of 4-sized, 6-sized and8-sized and macadam in thin layers. The short-term defense is to collectthe heavy rain water into the gully water transport mortise, and creeperplants are protected at the foot of the stack for long-term coverage andmaintenance; creeper plants are planted at the foot of the stack tospread the stack as a long-term cover, and when using, the roots of theplant are cut and burned with sulfuric acid, and then the net isuncovered by unmanned aerial vehicles after dried.

Thousands of embankment mortise stacks and implements, transporters canbe constructed to protect the defending party from the attacking ofrockets and missiles.

What is claimed is:
 1. An energy discharging implement in an open space for an energy carrying space device, the energy discharging implement comprising a fixed rod, an implement and an embankment mortise stack; wherein the fixed rod which is a top-down bracket supporting implement comprises a frame bracket rod with a base, a frame bracket rod, a bracket rod sleeve, a bracket top cover; the implement comprises a loading missile frame comprising a supporting shaft, a bearing sleeve, a support shaft bearing, a fixed bearing device, a bearing fixing nut, a guide rod, a guide rod bearing, a guide rod hanging piece, a diagonal sliding hole cover, a fixed hanging body, a frame bracket fixing plate, a frame bracket bottom plate, a spring narrow steel plate, a nylon rope net for picking up and changing the trajectory of thrown loading missiles, changed missiles, accepted cruise missiles, ballistic missiles and penetrating missiles; the embankment mortise stack comprises mixed mortises, slippery mortises and separation mortise boards; the mixed mortises are mortise stones covered on a surface of the stack with mortises with four diameters of φ12 cm, φ8 cm, φ4 cm, and wheat grain mortises which are layered orderly for 30 cm in each layer; the slippery mortises are mortise stones with φ12 cm and layered orderly in every layer of 3 m covered in the stack in the inner circle; the separation mortise board is a modular high-strength double-layer reinforced concrete slab or a high-strength fire-resistant glass steel sheets placed between different mortise layers; the stack is configured to catch missiles thrown by the loading missile frame or the missiles that are directly attacked; the set separation mortise boards in each layer have different seams and sizes, and right and left sides of each layer are asymmetric, and the set separation mortise boards in each layer which are not jointed are superimposed; the mortise sampan transporter further comprises mortise floating prying shoes, climbing claw shoes and covers; wherein the implement and the embankment mortise stack are integrated to collect rockets; structures and mechanisms of respective energy carrying devices fit surface tensions and friction coefficients of mortises, which consume energy of the energy carrying devices, so that the energy carrying devices are collected.
 2. The energy discharging implement of claim 1, wherein the energy discharging implement is manufactured by a method comprising the following steps: coating a bottom of the frame with a same resin and fiber cloth to double an original diameter of the frame when manufacturing the supporting shaft, so that the frame is reinforced to increase the missile throwing radian of the frame; hanging ropes with the same length at frame hanging rings below four corners of the frame, and fixing a resultant force object which is half of the frame in weight, so that everlasting operating is guaranteed due to floating of the frame; and manufacturing the guide rod with the same principle, wherein the remaining position in the wrap between the bearing, the bin, the hanging piece and axle is biased to the hanging piece to ensure that the missile striking the middle of the frame synchronously accepts the oblique displacement of the outer ring of the bearing and the rotating slide of the bearing load, and the hanging piece randomly decides directions.
 3. The energy discharging implement of claim 2, wherein the method for manufacturing the energy discharging implement further comprises the following steps: piling the rugged boards which are cast in-site in a staggered manner to reduce collapse of the embankment mortise stack which is not covered; enlarging an interface of the board to increase aggregation of the mortises; and forming the embankment mortise mountain through interaction of gaps of modular plates; fixing an initial mortise floating surface with the separation plates, smoothing the initial mortise floating surface, and covering a thick plastic film on the smoothed mortise floating surface; putting concrete onto the smoothed mortise floating surface, and then adding reinforcing bars onto the concrete; adding concrete onto the reinforcing bars and flattening; and then adding reinforcing bars and concrete on surface, and flattening; compressing with a rotary cylinder and consolidating with a plate type vibrator; curing, and cutting according to a requirement of set modules; or separating plates with wooden strips or grass ropes; casting modularly after covering a film, wherein the concrete is cast in layers.
 4. The energy discharging implement of claim 1, wherein the frame bracket fixed rod is obtained by compacting, reinforcing and strengthening a hollow rod, which improves a loading capacity of the implement and is used again after destroyed; after the loading missile frame is installed, sands with a high sedimentation rate from rivers are added into an upper opening of the frame bracket rod, and water is injected into the rod to promote settling; or mortar concrete or reinforced concrete is added into the opening of the frame bracket rod, and are vibrated by a vibrator, so that the loading and reuse capacity are improved.
 5. The energy discharging implement of claim 2, wherein the method further comprises the following steps: after the embankment mortise stack is constructed, covering the slope of the stack with a thin mixed layer of 2-sized, 4-sized, 6-sized and 8-sized stones which are used for buildings on a frontal surface, so that the mixed mortises on an outer surface are prevented from being washed away; planting ivies on the slope of the stack for a long-term curing; and cutting roots of the ivies and burning with sulfuric acids, and after withered, removing the ivies with an unmanned aerial vehicle.
 6. An energy discharging facility in an open space for an energy carrying space device, comprising a hidden mortise facility; wherein the hidden mortise facility comprises a modular scrap steel plate with an anti-rust treatment, a concrete rugged board or a glass steel rugged board for filling holes; attacking missiles are directly collected when a loading missile frame and a frame bracket fixed rod are removed; the mortise sampan facility further comprises mortise floating prying shoes, climbing claw shoes and covers; the facility and the embankment mortise stack are integrated to collect rockets; structures and mechanisms of respective energy carrying devices fit surface tensions and friction coefficients of mortises, which consume energy of the energy carrying devices, so that the energy carrying devices are collected.
 7. The energy discharging facility of claim 6, wherein the energy discharging facility is manufactured by a method comprising the following steps: casting the separation mortise boards; placing the waste steel plates which meet a requirement for modules on the mortise layer in a checkerboard manner after an anti-rust treatment; and casting rugged separation mortise plates, and filling the rugged separation mortise plates into vacancies, wherein sides of the steel plates may be thickened if necessary, so that a missile loading frame is removed in the hidden embankment mortise facility.
 8. The energy discharging facility of claim 7, wherein the method further comprises the following steps: after the embankment mortise stack is constructed, covering the slope of the stack with a thin mixed layer of 2-sized, 4-sized, 6-sized and 8-sized stones which are used for buildings on a frontal surface, so that the mixed mortises on an outer surface are prevented from being washed away; planting ivies on the slope of the stack for a long-term curing; and cutting roots of the ivies and burning with sulfuric acids, and after withered, removing the ivies with an unmanned aerial vehicle.
 9. An energy discharging transporter in an open space for an energy carrying space device, comprising a mortise sampan transporter; wherein the mortise sampan transporter comprises a mortise sampan, an acute angle pry plow (hammer) or a straight angle pry plow (hammer), a navigation hub, a storage lanyard; the mortise sampan comprises a loading rocket frame or a rocket changing frame, a frame bracket rod, an anti-reverse ring, an energy guide rod, an energy guide connecting rod, a sampan rudder, an energy guide wheel, an umbrella rib wheel, a sampan axle, a gasket, a bearing, a nut, a pin, a hoop, a sampan, and a floating mortise board of the travelling sampan with a sampan rudder ditch and a sling hole, a sampan tip, a sampan tip net and a sampan tip net fixing bracket rod; the acute angle pry plow (hammer) comprises a combination of an acute angle pry and a hammer with different rods, a hammer with same rods, a flat plow, a sharp plow, a bald plow; the straight angle pry plow (hammer) comprises a combination of a straight angle pry and a mortise draping rake, a mortise combing rake, a mortise separating hammer, a hammer with different rods or a hammer with short rods; the embankment mortise stack removes the separation mortise board, and the mortise sampan of the stack becomes a travelling sampan; a transfer of frictional energy is provided by lifting the acute angle pry plow (hammer) and the straight angle pry plow (hammer) segment by segment through a pre-positioned storage lanyard to collect a rocket in a set area, or the embankment mortise stack directly receives misguided rockets; the mortise sampan transporter further comprises mortise floating prying shoes, climbing claw shoes and covers; the facility and the embankment mortise stack are integrated to collect rockets; structures and mechanisms of respective energy carrying devices fit surface tensions and friction coefficients of mortises, which consume energy of the energy carrying devices, so that the energy carrying devices are collected.
 10. The energy discharging transporter of claim 9, wherein the energy discharging transporter is manufactured by a method comprising the following steps: continuously overlaying guides, energy consumption tools and plows to form an energy consumption mechanism, so that carrying energies of space rockets are consumed and space devices are collected without damage; manufacturing the anti-reverse ring, the energy guide rod and the energy guide wheel, wherein a total length of the energy guide rod and the energy guide wheel is slightly larger than a length between a bottom of the frame and a bottom of the sampan; molding the umbrella rib wheel with a thin edge and a thick hub, in which ribs of the umbrella rib wheel extend radially outward, and the thin edge of the umbrella rib wheel has no corners; manufacturing an acute angle pry and a hammer with different rods, a hammer with the same rods, a flat plow, a sharp plow, a bald plow to form the acute angle pry plow (hammer), or manufacturing a straight angle pry, and a mortise draping rake, a mortise combing rake, a mortise separating hammer, a hammer with different rods, a hammer with short rods to form the straight angle pry plow (hammer); placing one or more of the acute angle pry plow (hammer) and the straight angle pry plow (hammer) into the embankment mortise stack, wherein the separation mortise board is removed, and the pry plows (hammers) are associated with the mortise sampan using pre-positioned storage lanyards; mounting the energy guide rod, the energy guide wheel and the umbrella rib wheel at the mortise sampan; transmitting the energy to the energy guide rod and the stack bottom when impact of the rockets pushes the loading rocket frame to incline downwardly, so that the energy guide rod moves forwardly, and the energy guide wheel rolls forward to deliver part of the energy to the sampan tip, and at the same time, the sampan tip inclines downwardly to drive the sampan to move downwardly along a slope of the embankment mortise stack, and then the umbrella rib wheel moves against the mortises, and when the travelling sampan is stopped, the pre-positioned storage lanyards is exhausted, and the acute angle pry plow (hammer) or the straight angle pry plow(hammer) transmits frictions to the sampan to consume energy, so that the traveling sampan or the pry plow is collected when it is on the slope or near the ground.
 11. The energy discharging transporter of claim 10, wherein the method further comprises the following steps: after the embankment mortise stack is constructed, covering the slope of the stack with a thin mixed layer of 2-sized, 4-sized, 6-sized and 8-sized stones which are used for buildings on a frontal surface, so that the mixed mortises on an outer surface are prevented from being washed away; planting ivies on the slope of the stack for a long-term curing; and cutting roots of the ivies and burning with sulfuric acids, and after withered, removing the ivies with an unmanned aerial vehicle.
 12. The energy discharging transporter of claim 9, wherein mortise floating prying shoes are a walking tool on the mortise stone layer; a ratio of a size of pries to a size of shoes is 9:1, and the shoes are installed in a middle of the pries; the shoes and the pries are tightly jointed at a toe web position, and are loosely connected at a tendon position; climbing shoe covers and shows are used as an inspection protection tool, a ratio of a climbing shoe and a pry bottom of the climbing shoe is 1:5; a rear of the toe web position is arranged with multiple rows of long spikes which have a length of about 20 cm and penetrate through the pry; and the climbing claw covers are the same as mud tile board, and a ratio of a size of a pry board to a size of the mud tile board is 4:1, and multiple rows of long spikes which have a length of about 20 cm penetrate through the pry. 